Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes /

Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes / Daniel L. Sutliff and Clifford A. Brown, Bruce E. Walker.

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Bibliographic Details
Online Access: Online Access
Online Access
Main Authors: Sutliff, Daniel L. (Daniel Linden), 1962- (Author), Brown, Clifford A. (Clifford Alan) (Author), Walker, Bruce E. (Author)
Corporate Author: Fundamental Aeronautics Program (U.S.) (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2014.
Series:NASA technical memorandum ; 218119.
Subjects:
Acoustic properties.
Aerodynamic configurations.
Turbofan engines.
Ducts.
Aerodynamic noise.
Wind tunnel tests.
Description
Item Description:Title from title screen (viewed on Dec. 4, 2014)
"April 2014."
"Prepared for SciTech 2014 sponsored by the American Institute of Aeronautics and Astronautics, National Harbor, Maryland, January 13-17, 2014."
Physical Description:1 online resource (44 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 44)

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